東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Sliding mode control of a reusable l...

Hall, Charles E.

Linked to FindBook

Google Book

Amazon

博客來

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation./
Author:	Hall, Charles E.
Description:	143 p.
Notes:	Source: Masters Abstracts International, Volume: 43-03, page: 0899.
Contained By:	Masters Abstracts International43-03.
Subject:	Engineering, Aerospace. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1423592
ISBN:	0496112163

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.
Hall, Charles E.

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation. - 143 p.

Source: Masters Abstracts International, Volume: 43-03, page: 0899.

Thesis (M.S.E.)--The University of Alabama in Huntsville, 2005.

In this work, a flight control system for a reusable launch vehicle during Terminal Area Energy Management (TAEM), approach and landing phases of flight is developed and then tested in a high fidelity, nonlinear six degree of freedom simulation. A new control algorithm based on multiple time scale Sliding Mode Control, driven by sliding mode disturbance observers using gain adaptation is designed. Comparisons with a classical, gain scheduled PID controller are made and considerable improvements in performance are shown. The developed Sliding Mode Control system has potential to improve vehicle safety and reliability through robustness to disturbances, and to decrease development and operational cost by reduced analysis time and improved launch availability.

ISBN: 0496112163Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.
LDR:01607nmm 2200265 4500 001 1814813
005 20060719075937.5
008 130610s2005 eng d
020 $a 0496112163
035 $a (UnM)AAI1423592
035 $a AAI1423592
040 $a UnM $c UnM
100 1 $a Hall, Charles E. $3 1904262
245 1 0 $a Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.
300 $a 143 p.
500 $a Source: Masters Abstracts International, Volume: 43-03, page: 0899.
502 $a Thesis (M.S.E.)--The University of Alabama in Huntsville, 2005.
520 $a In this work, a flight control system for a reusable launch vehicle during Terminal Area Energy Management (TAEM), approach and landing phases of flight is developed and then tested in a high fidelity, nonlinear six degree of freedom simulation. A new control algorithm based on multiple time scale Sliding Mode Control, driven by sliding mode disturbance observers using gain adaptation is designed. Comparisons with a classical, gain scheduled PID controller are made and considerable improvements in performance are shown. The developed Sliding Mode Control system has potential to improve vehicle safety and reliability through robustness to disturbances, and to decrease development and operational cost by reduced analysis time and improved launch availability.
590 $a School code: 0278.
650 4 $a Engineering, Aerospace. $3 1018395
650 4 $a Applied Mechanics. $3 1018410
650 4 $a Engineering, Electronics and Electrical. $3 626636
690 $a 0538
690 $a 0346
690 $a 0544
710 2 0 $a The University of Alabama in Huntsville. $3 1017884
773 0 $t Masters Abstracts International $g 43-03.
790 $a 0278
791 $a M.S.E.
792 $a 2005
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1423592